Showing default

POSIDONIA, 69922

Orbit data source: Space-Track

POSIDONIA, 69922 is a Spanish payload satellite in SSO that was launched on Tue, 07 Jul 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
69922, 2026-156BF
Orbit
SSO
Country
Flag of ESES / SPN
Related business
None
Manufacturer
Open Cosmos
Mission
Operational spacecraft
Bus & Motor
OCOS, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
2026-07-07 (3 weeks ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
BOX, 0.4 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 POSIDONIA
1 69922U 26156BF  26211.27879661  .00000962  00000-0  10038-3 0  9998
2 69922  97.7507 111.3602 0009150  80.2400 279.9852 14.91980973  3420
Epoch: 2026-07-30T06:41Z
TLE epoch observation values (Epoch: 2026-07-30T06:41:28.027Z)
Latitude
0.00002°
Longitude
63.07182°
Altitude
593.701 km
Speed
7.564 km/s
True Right ascension
07h 25m 26s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
11:57:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.152 km
Perigee altitude
582.403 km
Semi-major axis
6,966.915 km
Eccentricity
0.00092
Inclination
97.7507°
RAAN
111.3602°
Arg. of periapsis
80.24°
True anomaly
279.88192°
Mean anomaly
279.9852°
Eccentric anomaly
279.93356°
Mean motion
3.73235 °/min
Orbital period
96.45 mins
BSTAR
0.00010038
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|